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A Perceptual Evaluation of the Efficacy of Sound Exposure Level in the Rating of Annoyance to Helicopter NoiseA psychoacoustic test was performed that aimed to test how well Sound Exposure Level (LAE) is at indicating changes in annoyance to helicopter noise for simple changes in design as well as for realistic changes found from flight tests. In particular, LAE was evaluated for auralizations of optimized designs of rotor geometries when compared to a baseline design and for recordings that compare different helicopters and maneuvers. Paired comparisons consisted of the 10dBA-down portion of flyovers, which is the same portion used to calculate LAE. When played at the same LAE, annoyance responses showed in which cases LAE is a good indicator as well as when other aspects not included in the calculation of LAE may be important. Annoyance responses for relative differences in LAE allowed the calculation of an Equal Annoyance Point, giving further insight to the performance of LAE. Confidence intervals calculated with Monte Carlo simulations showed when responses are statistically different from the equal LAE comparison and also gave an indication of the necessary reduction for designers to be confident that a low noise design is impactful or that a difference in rotorcraft or maneuver is perceptually favorable.
Document ID
20205008060
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Matthew Alban Boucher
(Langley Research Center Hampton, Virginia, United States)
Andrew William Christian
(Langley Research Center Hampton, Virginia, United States)
Siddhartha Krishnamurthy
(Langley Research Center Hampton, Virginia, United States)
Stephen A Rizzi
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
September 25, 2020
Subject Category
Acoustics
Report/Patent Number
TPSAS 34571
Meeting Information
Meeting: Vertical Flight Society Forum 76
Location: Virtual
Country: US
Start Date: October 6, 2020
End Date: October 8, 2020
Sponsors: VFS - The Vertical Flight Society
Funding Number(s)
WBS: 664817.02.07.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
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